This master’s thesis deals with the design of installation of floats for the M-4 Irbis airplane and it’s modification in aim to provide water level landing. Part of this thesis is selection of geometry of floats, weight analysis of the modified version and stress analysis of structural elements. The aim was to perform modification on a float plane which will have a minimal impact on the airframe and to meet the requirements of Certification Specification ASTM F2245 and CS-VLA. In conclusion, the hydrodynamic and aerodynamic characteristics including flight performance is determined. Final part is devoted to the design of the rudder for directional control of the floats.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:241712 |
| Date | January 2016 |
| Creators | Heczko, Nikodem |
| Contributors | Katrňák, Tomáš, Palička, Radek |
| Publisher | Vysoké učení technické v Brně. Fakulta strojního inženýrství |
| Source Sets | Czech ETDs |
| Language | Czech |
| Detected Language | English |
| Type | info:eu-repo/semantics/masterThesis |
| Rights | info:eu-repo/semantics/restrictedAccess |
Page generated in 0.0017 seconds